As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT C-CHECK, AFT FUSELAGE SECTION MAIN CARGO FLOOR SUPPORT ANGLE CRACKED AT STA 1723.000 RT. REMOVED DAMAGED AREA AND PERFORMED ANTI CORROSIVE TREATMENT IAW SRM 51-1-8 PAGE 11. INSTALLED EXTRUSION IAW SRM 53-2-0 PAGE 2E&F. SECURED EXTRUSION WITH CHERRY MAX RIVETS IAW SRM 51-1-21 PAGE 73. TREATED AND PRIMED IAW SRM 51-1-8 PAGE 35.